A low wake flow wing relates to aircraft wings. The low wake flow wing is provided with a left main wing and a right main wing which are fixed to the middle portion of an aircraft body. The left portion of the left main wing extends outside to form a left flap along the rear edge of the left main wing. The right portion of the right main wing extends outside to form a right flap along the rear edge of the right main wing. A left horizontal tail and a right horizontal tail are respectively mounted on both sides of a vertical tail on the rear portion of the aircraft body. The left main wing and the right main wing are in the same width and shape. The left flap and the right flap are in the same shape and width. The width of the left flap and the right flap is 35% to 65% of that of the left main wing and the right main wing. The left horizontal tail and the right horizontal tail are in the same shape and width. The width of the left horizontal tail and the right horizontal tail is 35% to 65% of that of the left main wing and the right main wing. The distance from the edges parallel to the axis of the aircraft body, of the left flap and the right flap to the tips of the left horizontal tail and the right horizontal tail is 0% to 10% of the width of the left main wing and the right main wing. The left flap and the right flap are triangular, are connected to the rear edges of the main wings on one side and are parallel to the axis of the aircraft body on the other side respectively.
Low wake flow wing
2015-04-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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